Bhavana, G N S and Singh, Suraj and Srinivas, G (2019) The numerical simulation and evaluation of aircraft engine axial flow turbine using numerical techniques. International Journal of Mechanical and Production, 9 (4). pp. 989-994. ISSN 2249-6890
![]() |
PDF
6952.pdf - Published Version Restricted to Registered users only Download (624kB) | Request a copy |
Abstract
This research aims to improve the efficiency of an axial flow turbine by improving the boundary conditions. In the baseline paper, Sherwood number, Nusselts number for a given flow were determined. The pressure ratio was not considered in the paper
Item Type: | Article |
---|---|
Uncontrolled Keywords: | Axial Flow Turbines, ANSYS Fluent, Sherwood Number, Nusselt Number, Tip Losses & Efficiency |
Subjects: | Engineering > MIT Manipal > Aeronautical and Automobile |
Depositing User: | MIT Library |
Date Deposited: | 24 Jul 2019 04:52 |
Last Modified: | 24 Jul 2019 04:52 |
URI: | http://eprints.manipal.edu/id/eprint/154226 |
Actions (login required)
![]() |
View Item |